FR2969577B1 - Aeronef muni d'un rotor arriere basculant, et procede associe - Google Patents
Aeronef muni d'un rotor arriere basculant, et procede associeInfo
- Publication number
- FR2969577B1 FR2969577B1 FR1005016A FR1005016A FR2969577B1 FR 2969577 B1 FR2969577 B1 FR 2969577B1 FR 1005016 A FR1005016 A FR 1005016A FR 1005016 A FR1005016 A FR 1005016A FR 2969577 B1 FR2969577 B1 FR 2969577B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- rotor
- associated method
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1005016A FR2969577B1 (fr) | 2010-12-22 | 2010-12-22 | Aeronef muni d'un rotor arriere basculant, et procede associe |
EP11009514.8A EP2468627B1 (fr) | 2010-12-22 | 2011-12-01 | Aéronef muni d'un rotor arrière basculant, et procédé associé |
US13/314,269 US8763949B2 (en) | 2010-12-22 | 2011-12-08 | Aircraft provided with a swiveling tail rotor, and an associated method |
CN201110452859.2A CN102530249B (zh) | 2010-12-22 | 2011-12-21 | 设有旋转尾桨的飞行器及相关联的方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1005016A FR2969577B1 (fr) | 2010-12-22 | 2010-12-22 | Aeronef muni d'un rotor arriere basculant, et procede associe |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2969577A1 FR2969577A1 (fr) | 2012-06-29 |
FR2969577B1 true FR2969577B1 (fr) | 2012-12-21 |
Family
ID=44305052
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1005016A Expired - Fee Related FR2969577B1 (fr) | 2010-12-22 | 2010-12-22 | Aeronef muni d'un rotor arriere basculant, et procede associe |
Country Status (4)
Country | Link |
---|---|
US (1) | US8763949B2 (fr) |
EP (1) | EP2468627B1 (fr) |
CN (1) | CN102530249B (fr) |
FR (1) | FR2969577B1 (fr) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8861879B2 (en) * | 2009-09-17 | 2014-10-14 | Samsung Electronics Co., Ltd. | Method and apparatus for encoding and decoding image based on skip mode |
WO2013105926A1 (fr) | 2011-03-22 | 2013-07-18 | Aerovironment Inc. | Aéronef réversible |
FR2977948B1 (fr) * | 2011-07-12 | 2014-11-07 | Eurocopter France | Procede de pilotage automatique d'un aeronef a voilure tournante comprenant au moins une helice propulsive, dispositif de pilotage automatique et aeronef |
US9505492B2 (en) | 2012-02-23 | 2016-11-29 | Sikorsky Aircraft Corporation | Mission adaptive rotor blade |
US9120567B2 (en) * | 2012-06-11 | 2015-09-01 | Sikorsky Aircraft Corporation | High speed compound rotary wing aircraft |
CN103057702B (zh) * | 2012-12-25 | 2016-05-18 | 天津全华时代航天科技发展有限公司 | 喷气式旋翼直升机 |
US9174730B2 (en) | 2013-08-21 | 2015-11-03 | Sikorsky Aircraft Corporation | Automated rotating tail rotor control |
FR3014837B1 (fr) * | 2013-12-17 | 2017-05-26 | Eurocopter France | Giravion equipe d'un rotor arriere anticouple participant a la sustentation du giravion par variation cyclique du pas des pales dudit rotor arriere |
FR3014838B1 (fr) | 2013-12-17 | 2015-12-25 | Eurocopter France | Giravion equipe d'un rotor arriere anti couple participant selectivement a la sustentation et a la propulsion en translation du giravion |
EP2899118B1 (fr) * | 2014-01-27 | 2019-01-16 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Hélicoptère comprenenat un fuselage et au moins un rotor principal |
US20170267338A1 (en) | 2014-10-01 | 2017-09-21 | Sikorsky Aircraft Corporation | Acoustic signature variation of aircraft utilizing a clutch |
US10822076B2 (en) | 2014-10-01 | 2020-11-03 | Sikorsky Aircraft Corporation | Dual rotor, rotary wing aircraft |
US10112697B2 (en) * | 2015-05-11 | 2018-10-30 | Sikorsky Aircraft Corporation | Aircraft with thrust vectoring tail |
US10167078B2 (en) * | 2015-09-21 | 2019-01-01 | Sikorsky Aircraft Corporation | Rotary or fixed wing aircraft with thrust vectoring tail |
US10703471B2 (en) | 2016-06-03 | 2020-07-07 | Bell Helicopter Textron Inc. | Anti-torque control using matrix of fixed blade pitch motor modules |
US10526085B2 (en) | 2016-06-03 | 2020-01-07 | Bell Textron Inc. | Electric distributed propulsion anti-torque redundant power and control system |
US10377479B2 (en) * | 2016-06-03 | 2019-08-13 | Bell Helicopter Textron Inc. | Variable directional thrust for helicopter tail anti-torque system |
CH713177A1 (de) * | 2016-11-21 | 2018-05-31 | Marenco Swisshelicopter Ag | Rotormast. |
US11186185B2 (en) | 2017-05-31 | 2021-11-30 | Textron Innovations Inc. | Rotor brake effect by using electric distributed anti-torque generators and opposing electric motor thrust to slow a main rotor |
US10831193B2 (en) * | 2017-11-14 | 2020-11-10 | Sikorsky Aircraft Corporation | Enhanced taxi control for rigid rotors |
FR3078945B1 (fr) | 2018-03-13 | 2022-05-06 | Innostar | Aerodyne hybride de type vtol ou stol (basculement rotor) |
US11203424B2 (en) * | 2019-03-13 | 2021-12-21 | The Boeing Company | Slewing mechanical power transmissions for rotorcraft |
CN109911218B (zh) * | 2019-03-13 | 2022-04-01 | 南京灵龙旋翼无人机系统研究院有限公司 | 一种用于旋转机翼飞机的多输入多输出动力系统及控制方法 |
US11279477B2 (en) * | 2019-03-19 | 2022-03-22 | Textron Innovations Inc. | Rotating electric distributed anti-torque fin |
US11230373B2 (en) * | 2019-12-02 | 2022-01-25 | Textron Innovations Inc. | Assembly and method for helicopter anti-torque |
US11554860B1 (en) * | 2020-06-23 | 2023-01-17 | Piasecki Aircraft Corporation | Apparatus, system and method for a convertible thruster for a compound aircraft |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE466905A (fr) * | ||||
GB599990A (en) | 1945-09-27 | 1948-03-25 | Cierva Autogiro Co Ltd | Improvements in helicopters |
FR1017976A (fr) * | 1947-07-27 | 1952-12-24 | Cierva Autogiro Co Ltd | Perfectionnement aux hélicoptères |
US2959373A (en) * | 1954-12-10 | 1960-11-08 | Daniel R Zuck | Convertiplane |
US3004736A (en) * | 1959-10-06 | 1961-10-17 | Lockheed Aircraft Corp | Tail rotor for helicopter |
US3155341A (en) * | 1963-04-05 | 1964-11-03 | Ryan Aeronautical Co | Convertiplane |
FR1511006A (fr) | 1966-12-13 | 1968-01-26 | Sud Aviation | Dispositif directionnel et propulsif pour hélicoptère |
FR1536412A (fr) | 1967-07-06 | 1968-08-16 | United Aircraft Corp | Mécanisme de commande de pivotement du rotor de queue d'un convertiplane |
US3540680A (en) * | 1968-05-24 | 1970-11-17 | Lockheed Aircraft Corp | Dual rotor system for helicopters |
US3977812A (en) * | 1975-11-17 | 1976-08-31 | The United States Of America As Represented By The Secretary Of The Army | Compound helicopter drive means |
US4759514A (en) * | 1986-09-30 | 1988-07-26 | The Boeing Company | Tail rotor yaw position control for a helicopter |
US4912999A (en) * | 1987-09-30 | 1990-04-03 | The Boeing Company | System for pivotably supporting and transmitting power through a helicopter transmission and rotor |
US5269654A (en) * | 1992-07-24 | 1993-12-14 | Don Chapman | Tail rotor assembly for helicopters |
US5749540A (en) * | 1996-07-26 | 1998-05-12 | Arlton; Paul E. | System for controlling and automatically stabilizing the rotational motion of a rotary wing aircraft |
FR2831934B1 (fr) | 2001-11-06 | 2004-01-16 | Eurocopter France | Boite de transmission basculante avec dispositif de rattrapage de jeu selon l'axe de basculement |
FR2831933B1 (fr) | 2001-11-06 | 2004-01-16 | Eurocopter France | Boite de transmission basculante a liaison pivotante a paliers lisses |
FR2831938B1 (fr) | 2001-11-07 | 2004-02-20 | Eurocopter France | Installation de lubrification pour boite de transmission de puissance basculante |
FR2842271B1 (fr) | 2002-07-15 | 2004-09-10 | Eurocopter France | Boite de transmissiion de puissance basculante a transfert de charge par le carter |
US6974105B2 (en) * | 2003-01-09 | 2005-12-13 | Roger N Pham | High performance VTOL convertiplanes |
US7137591B2 (en) | 2003-02-19 | 2006-11-21 | Cartercopters, L.L.C. | Tilting mast in a rotorcraft |
US8210468B2 (en) * | 2007-05-14 | 2012-07-03 | Blr Aerospace, L.L.C. | Aircraft stabilizer system and methods of using the same |
US8251305B2 (en) | 2008-02-13 | 2012-08-28 | Textron Innovations Inc. | Rotorcraft with variable incident wing |
-
2010
- 2010-12-22 FR FR1005016A patent/FR2969577B1/fr not_active Expired - Fee Related
-
2011
- 2011-12-01 EP EP11009514.8A patent/EP2468627B1/fr active Active
- 2011-12-08 US US13/314,269 patent/US8763949B2/en active Active
- 2011-12-21 CN CN201110452859.2A patent/CN102530249B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
US20120160954A1 (en) | 2012-06-28 |
CN102530249B (zh) | 2015-05-06 |
CN102530249A (zh) | 2012-07-04 |
FR2969577A1 (fr) | 2012-06-29 |
EP2468627B1 (fr) | 2016-03-02 |
US8763949B2 (en) | 2014-07-01 |
EP2468627A1 (fr) | 2012-06-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name |
Owner name: AIRBUS HELICOPTERS, FR Effective date: 20140602 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
ST | Notification of lapse |
Effective date: 20180831 |